AbstractA projectile which uses a bang-bang type guidance law is launched and its goal is to hit a fixed target whose center is located on the ground. In [1], applying stochastic control methods the performance of the projectile is investigated by using a point-mass model. In this work, which is a sequel to [1], a semirigid body model is used for the projectile and its performance is investigated by using stochastic control methods
This thesis report is focused on the design of a guidance and control system that is able to minimiz...
This paper proposes an optimal impact angle control guidance law for homing missiles with a narrow f...
The purpose of guidance is to cause a collision between a missile and a specified target. Accordingl...
AbstractA projectile which uses a bang-bang type guidance law is launched and its goal is to hit a f...
AbstractA projectile which uses a bang-bang type guidance law is launched, and its goal is to hit a ...
AbstractA projectile is analyzed which uses a bang-bang type guidance law with a wind stabilized see...
AbstractA projectile which uses a bang-bang type guidance law is considered. Two problems concerning...
The thesis traces the history of missile aerodynamic prediction methods and defines the aerodynamic ...
The dynamics of guided projectile systems are inherently stochas-tic in nature. While deterministic ...
This paper considers the problem of mimicking short-range ballistic trajectories and presents a feed...
In external ballistics of a conventional spin-stabilised artillery projectile, there are a numberof ...
Approved for public release; distribution unlimited. S,L By using more realistic a priori knowledge ...
The work in this thesis is on two topics. The first topic focuses on collaboration between a UAV and...
This article details the design of a pitch axis autopilot for an 80mm fin-stabilized, canard-guided ...
International audienceThis paper details the identification of a pitchaxis model for an 80-mm fin-st...
This thesis report is focused on the design of a guidance and control system that is able to minimiz...
This paper proposes an optimal impact angle control guidance law for homing missiles with a narrow f...
The purpose of guidance is to cause a collision between a missile and a specified target. Accordingl...
AbstractA projectile which uses a bang-bang type guidance law is launched and its goal is to hit a f...
AbstractA projectile which uses a bang-bang type guidance law is launched, and its goal is to hit a ...
AbstractA projectile is analyzed which uses a bang-bang type guidance law with a wind stabilized see...
AbstractA projectile which uses a bang-bang type guidance law is considered. Two problems concerning...
The thesis traces the history of missile aerodynamic prediction methods and defines the aerodynamic ...
The dynamics of guided projectile systems are inherently stochas-tic in nature. While deterministic ...
This paper considers the problem of mimicking short-range ballistic trajectories and presents a feed...
In external ballistics of a conventional spin-stabilised artillery projectile, there are a numberof ...
Approved for public release; distribution unlimited. S,L By using more realistic a priori knowledge ...
The work in this thesis is on two topics. The first topic focuses on collaboration between a UAV and...
This article details the design of a pitch axis autopilot for an 80mm fin-stabilized, canard-guided ...
International audienceThis paper details the identification of a pitchaxis model for an 80-mm fin-st...
This thesis report is focused on the design of a guidance and control system that is able to minimiz...
This paper proposes an optimal impact angle control guidance law for homing missiles with a narrow f...
The purpose of guidance is to cause a collision between a missile and a specified target. Accordingl...